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Kinetic Modeling of the Oxidation of Ammonia in Flames

1983/10/01 by James A. Miller, Mitchell D. Smooke, Robert M. Green +1 · 2 citations
Chemical Engineering · Engineering · Mathematics · #Advanced Combustion Engine Technologies #Combustion and flame dynamics #Gas Dynamics and Kinetic Theory

paper · doi:10.1080/00102208308923691

crossref issued 1983/10/01 · crossref published 1983/10/01 · crossref published-print 1983/10/01 · openalex publication_date 1983/10/01 · crossref published-online 2007/05/02 · crossref created 2007/06/25 · crossref deposited 2024/02/15 · openalex created_date 2025/10/10 · openalex updated_date 2026/08/03 · crossref indexed 2026/08/03

Abstract

We have investigated theoretically a variety of burner-stabilized and freely propagating NH3/2 and NH3/H2/2. flames. The agreement between theory and experiment is generally good except, perhaps, for very rich flames, where it appears that the kinetic model may be missing important pyrolysis steps. Nevertheless, the important NO and N2 formation reactions can be identified. In lean flames, nitric oxide is produced primarily through the nitroxyl (HNO intermediate, formed either by the reaction of NH2. with oxygen atoms or NH with hydroxyl and oxygen molecules. Similarly, in lcan flames conversion of NO to N2. is by reaction with NH2 or NH, forming NNH or N2.O as intermediates. Under richer conditions NH2.and NH are rapidly converted to nitrogen atoms, and the extended Zel'dovich mechanism becomes responsible for NO formation and the conversion of NO to N2. In addition to our analysis of the nitric oxide production and destruction paths, we find from a sensitivity analysis that the most important reaction in dutcrmining the flame speed under stoichiometric conditions is the chain branching reaction H | O3.⇌2OH+0. Other properties of the stoichiometric NH3-o2 flame worthy of mention are (I) a local maximum in the temperature profile (higher than the adiabatic Rame temperature) occurs in the interior of the flame, and (2) the flame speed is almost independent of pressure From 0.1 to 10 atmospheres.

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